US2295454A - Propeller blade - Google Patents

Propeller blade Download PDF

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Publication number
US2295454A
US2295454A US314907A US31490740A US2295454A US 2295454 A US2295454 A US 2295454A US 314907 A US314907 A US 314907A US 31490740 A US31490740 A US 31490740A US 2295454 A US2295454 A US 2295454A
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US
United States
Prior art keywords
blade
slab
board
laminated
propeller blade
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Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US314907A
Inventor
Cesare Pierino Di
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CESARE OFFSET PROPELLER CORP D
DI CESARE OFFSET PROPELLER Corp
Original Assignee
CESARE OFFSET PROPELLER CORP D
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by CESARE OFFSET PROPELLER CORP D filed Critical CESARE OFFSET PROPELLER CORP D
Priority to US314907A priority Critical patent/US2295454A/en
Application granted granted Critical
Publication of US2295454A publication Critical patent/US2295454A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
    • B64C11/20Constructional features
    • B64C11/22Solid blades

Definitions

  • the present invention relates to an improvement in propeller construction and more particularly to a novel blade construction and method of manufacture.
  • the blade is formed completely of wood laminations suitably impregnated and compressed to lform a compact unit having great inherent strength and adapted to give optimum elciency in use with a minimum of distortion under operating conditions.
  • the initial step consists in forming a laminated board of substantially rectangular shape and of substantially the ultimate or maximum length, Width and thickness of the body of the iinished propeller blade.
  • a separate strip or board of like material of such dimensions as to permit the ultimate forming of the shank of the blade in the most efficient and economicalv manner.
  • Fig. l is a viewY in end elevation of the finished blade.
  • Fig. 2 is a plan or elevational view thereof.
  • Fig. 3 is a series of views in vertical cross section'taken on the lines a-a, b--b, c-c, cf-d, e-e, -f and g--g of Figs. 1 and 2, respectively.
  • Fig. 4 is a fragmentary perspective view showing the laminated construction of the blade.
  • Fig. 5 is a view in end elevation of the 1aminated structure before the blade is formed.
  • Fig. 6 is a plan view of the laminated structure shown in Fig. 5.
  • Fig. 7 is a view in vertical cross section taken on the line l-l of Fig. 6.
  • Fig. 8 is an enlarged view in side elevation of the sheet or board to be attached to the main section to form the shank of the blade with the broken line showing where the cut is taken.
  • the novel propeller bladel is shown in Figs. 1 and 2 in its completed form afterlts blade surface and shank 2 have been turned down or contoured to the desired shape.
  • the shape of the blade being clearly shown in cross section in the composite view of Fig. 3.
  • the main board or slab 3 is shown of substantially rectangular form and of the ultimate dimensions of the body of the propeller blade.
  • ThisA board or slab is shown in Fig. 8 with the broken line 6 showing where the board or slab is c'ut to form the complementary sections. As shown in Figs. 6 and '7, these sections are of less Width than the board or body 3 of the blade and secured to this board in staggered relation, thus enactingv land, precise conformation with the master pattern.
  • the shank is rst turned to its proper dimensions and contour and the blade proper is then turned down in accordance with the contour thereof as shown in Figs. 1, 2 and 3.
  • the resultant blade is a compact and compressed laminated wood structure wholiy of compressed and treated wood having great inherent strength and maximum resistance to distortion or damage under operating conditions.
  • the laminated layers are preferably in the form of a relatively hardwood veneer impregnated v with a phenolforma1dehyde resin, after which a stack of suitable thickness of the ⁇ impregnated layers or sheets is placed into a heated press under extremely high pressure and squeezed or pressed into a fraction of its originalthickness. After the compressed board composed of a great to distortion or damage under operating conditions. comprising the steps of forming a rectangular slab ot laminated and resin impregnated wood.

Description

Sept. 8, 1942. P. Dl CESARE |J1+||||1|||||||||l+l CEE. T @E x w n Patented Sept. 8, `1942 UNITED STATES PATENT OFFICE PROPELLER BLADE Pierino Di Cesare, Oak Park, lll., assignor to Di Cesare Offset Propeller Corporation, Chicago, Ill., a corporation of Illinois I application January zz, 1940, serial No. 314,907
l Claim.
The present invention relates to an improvement in propeller construction and more particularly to a novel blade construction and method of manufacture.
In the novel embodiment disclosed in the drawing, the blade is formed completely of wood laminations suitably impregnated and compressed to lform a compact unit having great inherent strength and adapted to give optimum elciency in use with a minimum of distortion under operating conditions.
In the novel method of manufacture, the initial step consists in forming a laminated board of substantially rectangular shape and of substantially the ultimate or maximum length, Width and thickness of the body of the iinished propeller blade. To the opposite sides of this board is intimately attached, as by gluing or other suitable adhesive, a separate strip or board of like material of such dimensions as to permit the ultimate forming of the shank of the blade in the most efficient and economicalv manner.
'I'he shank and then the blade proper are turned down and contoured on a profile machine having a master pattern to permit the completed blade to be turned down or formed in single or simultaneous multiple units whereby to always assure accuracy and actual conformation with the master pattern.
Further objects are toprovide a construction of maximum simplicity, eillciency, economy and ease of assembly and operation, and such further objects, advantages and capabilities as will later more fully appear and are inherently possessed thereby.
The invention further resides in the construction, combination and arrangement of parts illustrated in the accompanying drawing, and while I have shown therein a preferred embodiment, it is to be understood that the same is susceptible of modification and change, and comprehends other details, arrangements of parts, features and constructions without departing from the spirit of the invention.
In the drawing:
Fig. l is a viewY in end elevation of the finished blade.
Fig. 2 is a plan or elevational view thereof.
Fig. 3 is a series of views in vertical cross section'taken on the lines a-a, b--b, c-c, cf-d, e-e, -f and g--g of Figs. 1 and 2, respectively.
Fig. 4 is a fragmentary perspective view showing the laminated construction of the blade.
Fig. 5 is a view in end elevation of the 1aminated structure before the blade is formed.
Fig. 6 is a plan view of the laminated structure shown in Fig. 5.
Fig. 7 is a view in vertical cross section taken on the line l-l of Fig. 6.
Fig. 8 is an enlarged view in side elevation of the sheet or board to be attached to the main section to form the shank of the blade with the broken line showing where the cut is taken.
Referring more particularly to the disclosure in the drawing, the novel propeller bladel is shown in Figs. 1 and 2 in its completed form afterlts blade surface and shank 2 have been turned down or contoured to the desired shape. the shape of the blade being clearly shown in cross section in the composite view of Fig. 3.
In preparing the laminated wood for turning, the main board or slab 3 is shown of substantially rectangular form and of the ultimate dimensions of the body of the propeller blade. To the opposite sides of this board or slab is securely amxed, as by gluing or the like, complementary sections 4, il of another board or slab 5. ThisA board or slab is shown in Fig. 8 with the broken line 6 showing where the board or slab is c'ut to form the complementary sections. As shown in Figs. 6 and '7, these sections are of less Width than the board or body 3 of the blade and secured to this board in staggered relation, thus enactingv land, precise conformation with the master pattern. In this turning operation, the shank is rst turned to its proper dimensions and contour and the blade proper is then turned down in accordance with the contour thereof as shown in Figs. 1, 2 and 3. The resultant blade is a compact and compressed laminated wood structure wholiy of compressed and treated wood having great inherent strength and maximum resistance to distortion or damage under operating conditions.
The laminated layers are preferably in the form of a relatively hardwood veneer impregnated v with a phenolforma1dehyde resin, after which a stack of suitable thickness of the `impregnated layers or sheets is placed into a heated press under extremely high pressure and squeezed or pressed into a fraction of its originalthickness. After the compressed board composed of a great to distortion or damage under operating conditions. comprising the steps of forming a rectangular slab ot laminated and resin impregnated wood. forming complementary strips of similar laminated and resin impregnated wood tapering in thickness from end to end and of less length and width than the rectangular slab, adhesively applying said strips to the opposite faces of the rectangular slab at one end thereof in such manner that the ends of said strips having the greatest thickness are Joined to the adjoining end of the in a hot oil bath for tempering the wood and providing a smooth, polished surface adapted towithstand continuous hard usage, give optimum eiliciency, and eliminate collection of condensate or moisture, thereby preventing ice formation on the blades.
Having thus disclosed the invention, I claim:
'I'he method of constructing a propeller blade of laminated wood impregnated with a resin and compressed to form a compact laminated wood blade of great inherent strength and resistance slab to form the thickened shank end of the propeller blade with a strip on one side of said rectangular slab having one of its longitudinal edges aligned with a longitudinal edge of the slab and a strip on the opposite side of said slab having one of its longitudinal edges aligned with the opposite edge of the slab, and forming the shank and finished blade from the composite slab and strips.
PIERINO DI CESARE.
US314907A 1940-01-22 1940-01-22 Propeller blade Expired - Lifetime US2295454A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US314907A US2295454A (en) 1940-01-22 1940-01-22 Propeller blade

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2423647A (en) * 1943-07-14 1947-07-08 Engineering & Res Corp Method of making articles of compressed and impregnated wood
US2634774A (en) * 1947-08-21 1953-04-14 Gordon J Francar Method of reconstructing unusable bowling pins
US2796215A (en) * 1952-08-19 1957-06-18 Cincinnati Testing & Res Lab Compressor blade and method of making
US3813842A (en) * 1969-10-17 1974-06-04 Trus Joist Corp Laminated, variable density, structural wood products and method for making the same
US4164061A (en) * 1977-08-24 1979-08-14 Bronovsky Grigory A Method of making rotor blades of radial-axial hydraulic machines

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2423647A (en) * 1943-07-14 1947-07-08 Engineering & Res Corp Method of making articles of compressed and impregnated wood
US2634774A (en) * 1947-08-21 1953-04-14 Gordon J Francar Method of reconstructing unusable bowling pins
US2796215A (en) * 1952-08-19 1957-06-18 Cincinnati Testing & Res Lab Compressor blade and method of making
US3813842A (en) * 1969-10-17 1974-06-04 Trus Joist Corp Laminated, variable density, structural wood products and method for making the same
US4164061A (en) * 1977-08-24 1979-08-14 Bronovsky Grigory A Method of making rotor blades of radial-axial hydraulic machines

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